What was found
AT C-CHECK, CRACK FOUND ON FUSELAGE SKIN AT STA 8.0, LONGERON 33. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER PER EO 97-53-0118, REPAIR 5 BY 3.5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, CRACK FOUND ON FUSELAGE SKIN AT STA 8.0, LONGERON 33. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER PER EO 97-53-0118, REPAIR 5 BY 3.5.